The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 27, 2024

Filed:

May. 11, 2023
Applicant:

Ratier-figeac Sas, Figeac, FR;

Inventors:

Julien Serieys, Lunan, FR;

Didier Delbruel, Prévinquières, FR;

Assignee:

RATIER-FIGEAC SAS, Figeac, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 31/04 (2006.01); G05G 1/01 (2008.04); G05G 1/04 (2006.01); G05G 5/00 (2006.01);
U.S. Cl.
CPC ...
B64D 31/04 (2013.01); G05G 1/01 (2013.01); G05G 1/04 (2013.01); G05G 5/005 (2013.01); G05G 2505/00 (2013.01);
Abstract

A throttle control lever suitable for controlling the magnitude and direction of thrust of one or more aircraft engines is described. The throttle control lever comprises a frame, a trigger mechanism, a connection element, a cam engagement mechanism, a biasing means, a cam, and a grip suitable for gripping by a user when the throttle control lever is in use, The cam comprises a slot having first and second slot portions and a stop portion. The stop portion extends between and connects the first and second slot portions. The cam engagement mechanism comprises a cam lever and a slot engagement element, the cam lever is pivotally attached to the frame via a cam lever pivot, and the slot engagement element is attached to the cam lever. The trigger mechanism comprises a trigger lever and a trigger, the trigger lever is pivotally attached to the frame via a trigger pivot.


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